| 54 |
Title |
TI |
[EN] Aircraft framework assembly, aircraft structural framework and aircraft with an aircraft structural framework |
| 71/73 |
Applicant/owner |
PA |
AIRBUS OPERATIONS GMBH, DE
|
| 72 |
Inventor |
IN |
BENTHIEN HERMANN, DE
;
KAISER NILS, DE
|
| 22/96 |
Application date |
AD |
Oct 19, 2018 |
| 21 |
Application number |
AN |
201816165245 |
|
Country of application |
AC |
US |
|
Publication date |
PUB |
Jun 1, 2021 |
33
31
32 |
Priority data |
PRC
PRN
PRD |
DE
102017219334
20171027
|
| 51 |
IPC main class |
ICM |
B64C 1/06
(2006.01)
|
| 51 |
IPC secondary class |
ICS |
F16B 7/18
(2006.01)
F16B 7/20
(2006.01)
|
|
IPC additional class |
ICA |
B33Y 80/00
(2015.01)
F16B 37/08
(2006.01)
F16B 5/02
(2006.01)
|
|
IPC index class |
ICI |
|
|
Cooperative patent classification |
CPC |
B33Y 80/00
B64C 1/061
B64C 1/064
B64C 1/065
B64C 1/069
F16B 37/085
F16B 5/0233
F16B 7/182
F16B 7/20
F16C 2326/43
F16C 7/02
|
|
MCD main class |
MCM |
B64C 1/06
(2006.01)
|
|
MCD secondary class |
MCS |
F16B 7/18
(2006.01)
F16B 7/20
(2006.01)
|
|
MCD additional class |
MCA |
B33Y 80/00
(2015.01)
F16B 37/08
(2006.01)
F16B 5/02
(2006.01)
|
| 57 |
Abstract |
AB |
[EN] A pole-shaped aircraft framework assembly including a first plug-and-turn connector forming a first end, a second plug-and-turn connector forming a second end, the second end opposite the first end, a first rod extending from the first plug-and-turn connector towards the second plug-and-turn connector, and a coupling component coupled to the second plug-and-turn connector for detachable coupling with the first rod. The first rod has a circumferential outer surface including alternately on a circumferential path in a cross-sectional plane of the first rod a ridged section and a plain section. The coupling component includes a tubular part having a circumferential inner surface including alternately on a circumferential path in a cross-sectional plane of the tubular part at least one ridged section and at least one plain section. One of the first rod and the coupling component is rotatable relative to the other one, engaging respective ridges of the first rod and the coupling component. |
| 56 |
Cited documents identified in the search |
CT |
US020170058959A1
US020170130766A1
US020170159700A1
US020180323493A1
US020180363689A1
|
| 56 |
Cited documents indicated by the applicant |
CT |
DE102015121018A1
EP000002766533B1
EP000003135833A1
EP000003254951A1
FR000002952146A1
US000009091387B2
US000009568040B2
US020090218777A1
US020170235062A1
|
| 56 |
Cited non-patent literature identified in the search |
CTNP |
|
| 56 |
Cited non-patent literature indicated by the applicant |
CTNP |
Extended European Search Report for Application No. 18200875.5 dated Apr. 10, 2019. 1;
German Search Report for German Application No. 10 2017 219 334.4 dated Feb. 14, 2018. 1;
Interview Summary for European Application No. 18200875.5 dated Dec. 20, 2019. 1
|
|
Citing documents |
|
Determine documents
|
|
Sequence listings |
|
|
|
Search file IPC |
ICP |
B64C 1/06
F16B 37/08
F16B 5/02
F16B 7/18
F16B 7/20
|
